Discussion Overview
The discussion revolves around the calculation of thrust generated by a tank under pressure, specifically focusing on the implications of removing a square inch from the tank's end and how this affects the force exerted in the opposite direction. The conversation includes theoretical considerations, practical testing scenarios, and comparisons between using air and water as the working fluid.
Discussion Character
- Exploratory
- Technical explanation
- Debate/contested
- Experimental/applied
Main Points Raised
- Some participants propose that removing a square inch from a tank with 1000 psi creates a pressure differential that results in a 1000 lb force pushing in the opposite direction.
- Others argue that according to Newton's Third Law, if there is a 1000 lb force on the removed area, there must be an equal reaction force on the tank.
- A participant draws a parallel between the thrust generation in rockets and the pressure dynamics in the tank, suggesting that the combustion chamber acts similarly to a high-pressure tank.
- There is a discussion about the practical differences between using air and water in the tank, with some noting that maintaining pressure with air requires moving a larger volume compared to water.
- One participant shares details about their testing setup, including the pressures and equipment used, and expresses curiosity about expected thrust values in different scenarios.
- Another participant highlights the importance of kinetic energy in the context of thrust generation, suggesting that compressed air may be more suitable for applications requiring energy storage.
- There is a question regarding the direction of thrust and its relevance to the intended application, indicating that the design may influence the choice of fluid used.
Areas of Agreement / Disagreement
Participants express differing views on the implications of pressure changes in the tank and the resulting thrust. While some agree on the basic principles of thrust generation, there is no consensus on the specifics of the calculations or the practical outcomes of the tests being discussed.
Contextual Notes
Participants mention various assumptions, such as the need for constant pressure maintenance and the differences in energy storage between compressed air and liquids. The discussion also reflects uncertainty regarding the actual thrust values that may be achieved in practice.